Air separation system and method with modulated warning flow

Abstract

An inerting system and method characterized by a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a secondary air separation module configured to communicate with the upstream source of pressurized air at elevated temperature for production of a supplemental downstream flow of nitrogen-enriched air to be delivered to a space to be inerted when high nitrogen-enriched airflow is desired during a high flow period; and a flow controller configured to provide a warming flow through the secondary air separation module to heat the secondary air separation module to above ambient temperature during a warming period other than the high flow period.

Description

RELATED APPLICATION DATA[0001]This application claims the benefit of U.S. Provisional Application No. 60 / 503,813 filed Sep. 22, 2003, which is hereby incorporated herein in its entirety.FIELD OF THE INVENTION[0002]The invention herein described relates generally to air separation systems and methods and particularly those that supply nitrogen enriched air to spaces to be inerted, such as the ullage space in an aircraft fuel tank.BACKGROUND OF THE INVENTION[0003]Aircraft have used on-board inert gas generating systems (OBIGGS) to protect against fuel tank explosions by replacing the potentially explosive fuel vapor / air mixture above the fuel in the ullage space of the tanks with nitrogen-enriched air (NEA). The NEA is generated by separating oxygen from local, ambient air and pumping the inert, oxygen impoverished NEA into the tanks.[0004]Production of NEA typically is carried out by means of an apparatus relying on permeable membranes, or else on molecular sieves. The air separation...

AI Technical Summary

Benefits of technology

[0007]The present invention provides an air separation system and method wherein a warming flow through one or more of the secondary ASMs is modulated to provide for improved efficiency of the secondary ASMs when high purity NEA flow is desired, as during aircraft descent.

[0016]According to another aspect of the invention, an inerting method comprising the steps of using a primary air separation module for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; using a secondary air separation module for production of a supplemental downstream flow of nitrogen-enriched air to be delivered to a space to be inerted when high nitrogen-enriched air flow is desired during a high flow period; and providing a warming flow of pressurized air at elevated temperature through the secondary air separation module to heat the secondary air separation module to above ambient temperature during a warming period other than the high flow period.

Problems solved by technology

This use of engine bleed air can decrease engine performance and can lead to increased fuel consumption.

The secondary ASMs, however, are idle, i.e. shut off from the elevated temperature supply air, and can become thermally soaked at surrounding ambient bay temperatures considerably lower than the optimal operating temperature of the ASM.

Consequently, when the pressurized heated supply air is supplied to the secondary ASMs for high NEA flow during descent, initially the secondary ASMs will not be at the desired elevated temperature and thus will produce low purity NEA.

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